General Electric Company
Airfoil with cooling circuit

Last updated:

Abstract:

An airfoil for a turbine engine having an engine component including an internal cooling circuit fluidly coupled to a plurality of passages within the outer wall of the engine component where cooling air moves from the internal cooling circuit to an outer surface of the engine component through the passages.

Status:
Grant
Type:

Utility

Filling date:

10 May 2016

Issue date:

23 Jul 2019